Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte.

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Bibliographic Details
Main Author:	Hussaini, M. Moin
Corporate Author:	Langley Research Center
Other Authors:	Korte, John J.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1996]
Series:	NASA technical memorandum ; 110295.
Subjects:	Navier-Stokes equations. Rockets (Aeronautics) > Nozzles. Computational fluid dynamics. Navier-Stokes equation. Nozzle design. Rocket nozzles. Low Reynolds number. Nozzle thrust coefficients.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:110295
NAS 1.15:110295	Restricted Place a Hold